View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 63114U 26145.09384315 +.00000000 +00000-0 +12443-2 0 00005
2 63114 43.0005 136.1467 0001728 267.6743 92.3927 15.70830958 08
| Epoch (UTC): | 25 May 2026 02:15:08 |
| Eccentricity: | 0.0001728 |
| inclination: | 43.0005° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 136.1467° |
| argument of perigee: | 267.6743° |
| revolutions per day: | 15.70830958 |
| mean anomaly at epoch: | 92.3927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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